[1] 欧阳自远.月球探测的进展与中国的月球探测[J].地质科技情报,2004,23(4):1-5. [Ouyang Z Y. International lunar exploration progress and Chinese lunar exploration[J]. Geological Science and Technology Information, 2004,23(4):1-5.]
[2] 邓连印,崔乃刚.月球探测发展历程及启示[J].哈尔滨工业大学学报:社会科学版,2008,10(3):14-19.[Deng L Y, Cui N G. The development and enlightenment of lunar exploration[J]. Journal of Harbin Institute of Technology (Social Sciences Edition), 2008,10(3):14-19.]
[3] Chory M A, Hoffman D P, LeMay J L. Satellite autonomous navigation-status and history[C]//Position Location and Navigation Symposium.[S. l.]:[s. n.], 1986:110-121.
[4] Chory M A, Hoffman D P, Major C S, et al. Autonomous navigation-where we are in 1984[C]//Proceedings of the AIAA Guidance and Navigation Symposium.[S. l.]: AIAA, 1984:27-36.
[5] Mendell W W, Heydorn R P. Lunar precursor missions for human exploration of Mars-III: studies of system reliability and maintenance[J]. Acta Astranautica, 2004(55):773-780.
[6] KTakashi K, Yoji K, Yasuharu K, et al. Small light-weight rover "Micro 5" for lunar exploration[J]. Acta Astronautica, 2003(52):447-453.
[7] Elfving A, Stagnaro L, Winton A. SMART-1: key technologies and autonomy implementations[J]. Acta Astronautica, 2003(52):475-486.
[8] Foing B H, Racca G D, Marini A, et al. SMART-1: mission to the moon: technology and science goals[J]. Advances in Space Research, 2003,1(11):2323-2333.
[9] Ouyang Z Y. Scientific objectives of Chinese lunar exploration project and development strategy[J]. Advance in Earth Sciences, 2004,19(3):351-359.
[10] 郗晓宁,曾国强,任萱,等.月球探测器轨道设计[M].北京:国防工业出版社,2001. [Xi X N, Zeng G Q, Ren X, et al. Design of lunar probe trajectory[M]. Beijing: National Defense Industry Press,2001.]
[11] 林胜勇.月球探测器轨道设计和计算[D].西安:西北工业大学,2005. [Lin S Y. Design and computation of lunar probe trajectory[D]. Xi'an: Northwestern Polytechnical University, 2005.]
[12] 王大轶,李铁寿,严辉,等.月球引力转弯软着陆的制导控制研究[J].中国空间科学技术,2000(5):17-23. [Wang D Y, Li T S, Yan H,et al. Guidance control for lunar gravity-turn descent[J]. Chinese Space Science and Technology, 2000(5):17-23.]
[13] 王大轶.月球软着陆的制导控制研究[D].哈尔滨:哈尔滨工业大学, 2000. [Wang D Y. Guidance control of lunar soft landing[D]. Harbin: Harbin Institute of Technology, 2000.]
[14] 王劼,崔乃刚,刘暾.通过"建立月球垂线"实现月球软着陆方法研究[J].导弹与航天运载技术,2000(4):45-47. [Wang J, Cui N G, Liu D. Study on lunar soft landing by the method of establishment of the lunar perpendicular[J]. Missiles and Space Vehicles, 2000(4):45-47.]
[15] Bennett F V. Apollo experience report mission planning for lunar module descent and ascent[R]. National Aeronautics and Space Administration, NASA-TN-D-6846, 1972.
[16] Moesser T J. Guidance and navigation linear covariance analysis for lunar powered descent[D]. Utah State University, 2010.
[17] Klumpp A R. Apollo lunar descent guidance[J]. Automatica, 1974(10):133-146.
[18] Boere M. Optimization of descent trajectories for lunar base settlement[D]. Delft: Delft University of Technology, 2010.
[19] Parsley J. Near-optimal feedback guidance for an accurate lunar landing[D]. University of Alabama, 2012.
[20] 孙泽州,贾阳,张熇.嫦娥三号探测器技术进步与推动[J].中国科学:技术科学,2013,43(11):1186-1192. [Sun Z Z, Jia Y, Zhang H. Technological advancements and promotion roles of Chang'e-3 lunar probe mission[J]. Sci Sin Tech, 2013,43(11):1186-1192.]
[21] 张洪华,关轶峰,黄翔宇,等.嫦娥三号着陆器动力下降的制导导航与控制[J].中国科学:技术科学,2014,44(4):377-384. [Zhang H H, Guan Y F, Huang X Y, et al. Guidance navigation and control for Chang'E-3 powered descent[J]. Sci Sin Tech, 2014,44(4):377-384.]
[22] 孙泽州,张熇,贾阳.嫦娥三号探测器地面验证技术[J].中国科学:技术科学,2014,44(4):369-376. [Sun Z Z, Zhang H, Jia Y, et al. Ground validation technologies for Chang'E-3 lunar spacecraft[J]. Sci Sin Tech, 2014(44):369-376.]
[23] 沈祖炜.阿波罗登月舱最终下降及着陆综述[J].航天返回与遥感,2008,29(1):11-14. [Shen Z W. The survey of Apollo LM during the descent to the lunar surface[J]. Spacecraft Recovery & Remote Sensing, 2008,29(1):11-14.]
[24] 和兴锁,林胜勇,张亚峰.月球探测器直接软着陆最优轨道设计[J].宇航学报,2007,28(2):409-413. [He X S, Lin S Y, Zhang Y F. Optimal design of direct soft-landing trajectory of lunar prospector[J]. Journal of Astronautics, 2007,28(2):409-413.]
[25] Sostaric R R, Rea J R. Powered descent guidance methods for the moon and mars[C]//AIAA Guidance, Navigation, and Control Conference and Exhibit.[S. l.]: AIAA,2005.
[26] 褚桂伯,张熇.月球探测器技术[M].北京:中国科学技术出版社,2007. [Chu G B, Zhang H. Lunar probe technology[M]. Beijing: China Science and Technology Press, 2007.]
[27] Mizuno T, Saito H, Ichikawa M. Communication system and operation for lunar probes under lunar surface[J]. IEEE Transactions On Aerospace and Electronic Systems, 2000,36(1):151-162.
[28] 王大轶,李铁寿,马兴瑞.月球探测器重力转弯软着陆的最优制导[J].自动化学报,2002,28(3):385-390. [Wang D Y, Li T S, Ma X R. Optimal guidance for lunar gravity-turn descent[J]. ACTA Automatica Sinica, 2002,28(3):385-390.]
[29] 朱建丰,徐世杰.月球重力转弯软着陆的模糊变结构控制[J].北京航空航天大学学报,2007,33(5):539-543.[Zhu J F, Xu S J. Fuzzy variable structure control for lunar gravity-turn landing[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007,33(5):539-543.]
[30] Jungmann J A. The exact analytic solution of the lunar landing problem[J]. AAS Sciences and Technology Seiries, 1967(11):381-397.
[31] Feng T Y, Wasynczuk C A. Terminal guidance for soft and accurate lunar landing for unmanned spacecraft[J]. Journal of Spacecraft and Rocket, 1968,5(6):644-648.
[32] Mcinnes C R. Nonlinear transformation methods for gravity-turn descent[J]. Journal of Guidance, Control and Dynamics, 1995,19(1):241-248.
[33] 江秀强,谭飞.深空软着陆制导控制的建模与仿真[J].四川理工学院学报:自然科学版,2010,23(5):608-612.[Jiang X Q, Tan F. Modeling and simulation on the guidance and control in deep-space soft landing[J]. Journal of Sichuan University of Science & Engineering (Natural Science Edition), 2010,23(5):608-612.]
[34] Wang J, Cui N G, Liu D. Study on lunar soft landing by the method of establishment of the lunar perpendicular[J]. Missiles and Space Vehicles, 2000,4:45-47.
[35] Citron S J, Dunin S E, Messinger H F. A terminal guidance technique for lunar landing[J]. AIAA Journal, 1964,2(3):503-509.
[36] Kian Y, Ernst M. Analysis of parking orbits and transfer trajectories for mission design of cis-lunar space stations[J]. Acta Astronautica, 2004,55:759-771.
[37] Siegfried W H. Lunar base development missions[J]. Acta Astronautica, 1999,44:755-767.
[38] Nagarajan N, Seetharama M, Kasturirangan K. Modified kalman filter based autonomous orbit determination using horizon scanner measure-ments[J]. Acta Astronautica, 1996,38(10):769-782.
[39] Knezevic Z, Milani A. Orbit maintenance of a lunar polar orbiter[J]. Planet and Space Science, 1998,46(11):1605-1611.
[40] Cheng R K, Meredith C M. Design considerations for surveyor guidance[J]. Journal of Spacecraft and Rockets, 1966,11:1569-1576.
[41] 王大轶,李铁寿,严辉,等.月球软着陆的神经元最优制导控制方法[J].系统工程与电子技术,1999,21(12):31-36.[Wang D Y, Li T S, Yan H, et al. Neuro-optimal guidance law for lunar soft landing[J]. Systems Engineering and Electronics, 1999,21(12):31-36.]
[42] 江秀强.基于IMU/LIDAR的月面软着陆自主导航方法[J].导弹与航天运载技术,2013(4):56-60.[Jang X Q. Autonomous navigation based on inertial measurement unit and light detection and ranging for lunar soft landing[J]. Missiles and Space Vehicles, 2013(4):56-60.]
[43] Bennett F V. Lunar descent and ascent trajectories[C]//AIAA 8th Aerospace Sciences Meeting.[S. l.]:AIAA,1970.
[44] Liu X L, Duan G R. Nonlinear optimal control for the soft landing of lunar landers[J]. Journal of ] Brady T, Paschall S. The challenge of sa剦浥攠l杵瑮轡睲阠乬剡剮此剩孮乧捛剃敝氯砯穉EEE 呁履湲o味屰湡嵣乥夠孃onference,[S. l.]:[s. n.] 2010.
[45] Liu Z Q, Di K C, Peng M, et al. High precision landing site mapping and rover localization for Chang'e-3 mission[J]. Science China Physics, Mechanics & Astronomy, 2015,58(1):1-11.
[46] Huang Y, Chang S Q, Li P J, et al. Orbit determination of Chang'e-3 and positioning of the lander and the rover[J]. Chinese Science Bulletin, 2014,59:3858-3867. landings[J]. Navigation, 1994,41(2):215-228.
[47] Souza C N. An optimal guidance law for planetary landing[C]//Proceedings of AIAA GNC Conference. [S. l.]: AIAA, 1997.
[48] Ueno S, Yamaguchi Y. Near minimum fuel guidance law of a lunar landing Module[C]//Proceedings of 14th IFAC Symposiumon Automatic Control in Aerospace.[S. l.]:[s. n.],1998: 377-382.
[49] Finzi A E, Gilardi G, Alippi S, et al. Automatic optimum moon landing[C]//Proceedings of 48th International Astronautical Congress, IAF2972.[S. l.]:[s. n.],1997.
[50] Guo J, Han C. Design of guidance laws for lunar pinpoint soft landing[C]//AAS/AIAA Astrodynamics Specialist Conference.[S. l.]: AIAA, 2009:2133-2145.
[51] 李爽,彭玉明,刘宇飞.星际着陆自主障碍检测与规避技术[J].航空学报,2010,31(8):1584-1592. [Li S, Peng Y M, Liu Y F. Autonomous obstacle detection and avoidance for planetary landing[J]. Acta Aeronautica et Astronautica Sinica, 2010,31(8):1584-1592.]
[52] 陈忠贵.小型月球探测器系统总体技术研究报告[R].863项目研究报告,1998:5-29. [Chen Z G. The overall technical research report of the small lunar probe system[R]. Research report of 863 project, 1998:5-29.]
[53] Parreira B, Vasconcelos J F, Montao J, et al. Hazard detection and avoidance in ESA lunar lander: concept and performance[C]//AIAA Guidance, Navigation, and Control (GNC) Conference.[S. l.]: AIAA,2013.
[54] Epp C D, Smith T B. Autonomous precision landing and hazard detection and avoidance technology (ALHAT)[C]//IEEE Aerospace Conference. [S. l.]: IEEE, 2007.
[55] Li S, Peng Y M. Autonomous hazard detection and avoidance for safe planetary landing[C]//61st International Astronautical Congress.[S.l.]:[s.n.], 2010.
[56] Uchiyama1 K. Guidance law for lunar lander with input constraint[C]//AIAA Guidance, Navigation and Control Conference and Exhibit.[S.l.]: AIAA, 2007.
[57] 黄翔宇,张洪华,王大轶,等."嫦娥三号" 探测器软着陆自主导航与制导技术[J].深空探测学报,2014,1(1):52-59. [Huang X Y,Zhang H H,Wang D Y,et al. Autonomous navigation and guidance for Chang'e-3 soft landing[J]. Journal of Deep Space Exploration, 2014,1(1):52-59.]
[58] Hamada Y, Ninomiya T, Katayama Y, et al. Feasibility study for precise lunar landing using SELENE-B lander configuration[R]. JAXA Research and Development Report, JAXA-RR-05-013E, 2005.
[59] 蔡艳芳.月球探测器软着陆制导控制方法研究[D].西安:西北工业大学,2006. [Cai Y F. A study of the guidance and control strategy in lunar soft-landing[D]. Xi'an: Northwestern Polytechnical University, 2006.]
[60] NASA Manned Spacecraft Center. Apollo 11 mission report[R]. NASA TM-X-62633, 1969.
[61] NASA Johnson Space Center. Apollo 12 mission report[R]. NASA TM-X-74200, 1970.
[62] NASA Manned Spacecraft Center. Apollo 14 mission report[R]. NASA TM-X-74240, 1971.
[63] NASA Manned Spacecraft Center. Apollo 15 mission report[R]. NASA TM-X-68394, 1971.
[64] NASA Manned Spacecraft Center. Apollo 16 mission report[R]. NASA TM-X-68635, 1972.
[65] NASA Johnson Space Center. Apollo 17 mission report[R]. NASA TM-X-69292, 1973.
[66] Davies M E, Colvin T R. Lunar coordinates in the regions of the Apollo landers[J]. Journal of Geophysical Research, 2000,105(E8):20277-20280.
[67] NASA Lunar and Planetary Program Division. Surveyor program results[R]. NASA SP-184, 1969.
[68] Ribarich J J. Surveyor spacecraft landing accuracy[J]. Journal of Spacecraft and Rockets, 1968,5(7):768-773.
[69] Siddiqi A A. Challenge to Apollo: the Soviet Union and the space race 1945~1974[R]. NASA SP-2000-4408, 2000.
[70] Shkuratov Y, Kaydash V, Sysolyatina X, et al. Lunar surface traces of engine jets of Soviet sample return probes: the enigma of the luna-23 and luna-24 landing sites[J]. Planetary and Space Science, 2013,75:28-36.
[72
